Analysis and Compensation of Modulation Angular Rate Error Based on Missile-Borne Rotation Semi-Strapdown Inertial Navigation System

The Semi-Strapdown Inertial Navigation System (SSINS) provides a new solution to attitude measurement of a high-speed rotating missile. However, micro-electro-mechanical-systems (MEMS) inertial measurement unit (MIMU) outputs are corrupted by significant sensor errors. In order to improve the naviga...

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Detalles Bibliográficos
Autores principales: Zhang, Jiayu, Li, Jie, Zhang, Xi, Che, Xiaorui, Huang, Yugang, Feng, Kaiqiang
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2018
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC5981495/
https://www.ncbi.nlm.nih.gov/pubmed/29734707
http://dx.doi.org/10.3390/s18051430

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC5981495/
https://www.ncbi.nlm.nih.gov/pubmed/29734707
http://dx.doi.org/10.3390/s18051430

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